Cessna 150, AVIONICS SUPPORT EQUIPMENT Cessna 150 full training course,

 

WELCOME ADVANCE FLYING ACADEMY 


AVIONICS SUPPORT EQUIPMENT

The airplane may, at the owner's discretion, be equipped with various types of avionics support equipment such as an audio control panel and static dischargers. The following paragraphs discuss these items.

AUDIO CONTROL PANEL

Operation of radio equipment is covered in Section 9 of this handbook.

When one or more radios is installed, a transmitter/audio switching system is provided The operation of this switching system is described in the following paragraphs.

The transmitter selector switch is labeled TRANS, and has two positions. When two transmitters are installed, it is necessary to switch the

microphone to the radio unit the pilot desires to use for transmission. This is accomplished by placing the transmitter selector switch in the position corresponding to the radio unit which is to be used. The up position selects the upper transmitter and the down position selects the lower transmitter.

The installation of Cessna radio equipment provides certain audio back-up capabilities and transmitter selector switch functions that the pilot should be familiar with. When the transmitter selector switch is placed in the No. 1 or No. 2 position, the audio amplifier of the corresponding transceiver is utilized to provide the speaker audio for all radios. If the audio amplifier in the selected transceiver fails, as evidenced by loss of speaker audio for all radios, place the transmitter selector switch

in the other transceiver position. Since an audio amplifier is not utilized for headphones, a malfunctioning amplifier will not affect headphone operation.

The speaker-phone switches determine whether the output of the receiver in use is fed to the headphones or through the audio amplifier to the speaker. Place the switch for the desired receiving system either in the up position for speaker operation or in the down position for headphones. The center OFF position will remove receiver output to either headphones or the speaker.

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👉 CRUISE

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👉 ENGINE

👉 PROPELLER

👉 MAXIMUM CERTIFICATED WEIGHTS

👉 STANDARD AIRPLANE WEIGHTS

👉 POWER PLANT LIMITATIONS

👉 FUEL & OIL CAPACITY

👉 INSTRUMENT PANEL VOCABULARY

👉 WEIGHT LIMITS

👉 CENTER OF GRAVITY LIMITS

👉 MANEUVER LIMITS

👉 FLIGHT LOAD FACTOR LIMITS

👉 KINDS OF OPERATION LIMITS

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👉 ENGINE FAILURE DURING TAKEOFF RUN

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👉 DITCHING

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👉 ENGINE FIRE IN FLIGHT

👉 ELECTRICAL FIRE IN FLIGHT

👉 CABIN FIRE

👉 WING FIRE

👉 INADVERTENT ICING ENCOUNTER

👉 LANDING WITH A FLAT MAIN TIRE

👉 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS

👉 AMMETER SHOWS DISCHARGE

👉 ENGINE FAILURE

👉 FORCED LANDINGS

👉 LANDING WITHOUT ELEVATOR CONTROL

👉 FIRES

👉 EMERGENCY OPERATION IN CLOUDS

👉 EXECUTING A 180° TURN IN CLOUDS

👉 EMERGENCY DESCENT THROU GH CLOUDS

👉 RECOVERY FROM A SPIRAL DIVE

👉 FLIGHT IN ICING CONDITIONS

👉 SPINS

👉 CARBURETOR ICING

👉 SPARK PLUG FOULING

👉 MAGNETO MALFUNCTION

👉 LOW OIL PRESSURE

👉 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS

👉 EXCESSIVE RATE OF CHARGE

👉 INSUFFICIENT RATE OF CHARGE

👉 NOISE ABATEMENT

👉 AIRFRAME

👉 FLIGHT CONTROLS

👉 TRIM SYSTEM

👉 INSTRUMENT PANEL

👉 GROUND CONTROL

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👉 ENGINE INSTRUMENTS

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👉 IGNITION-STARTER SYSTEM

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👉 EXHAUST SYSTEM

👉 CARBURETOR AND PRIMING SYSTEM

👉 COOLING SYSTEM

👉 BRAKE SYSTEM

👉 ELECTRICAL SYSTEM

👉 OVER-VOLTAGE SENSOR AND WARNING LIGHT

👉 CIRCUIT BREAKERS AND FUSES

👉 GROUND SERVICE PLUG RECEPTACLE

👉 EXTERIOR LIGHTING

👉 INTERIOR LIGHTING

👉 VENTILATING AND

DEFROSTING SYSTEM

👉 PITOT-STATIC SYSTEM AND INSTRUMENTS

👉 AIRSPEED INDICATOR

👉 RATE-OF-CLIMB INDICATOR

👉 ALTIMETER

👉 VACUUM SYSTEM AND INSTRUMENTS

👉 ATTITUDE INDICATOR

👉 DIRECTIONAL INDICATOR

👉 SUCTION GAGE

👉 STALL WARNING SYSTEM

👉 AVIONICS SUPPORT EQUIPMENT

👉 STATIC DISCHARGERS

👉 IDENTIFICATION PLATE

👉 OWNER FOLLOW-UP SYSTEM

👉 PUBLICATIONS

👉 AIRPLANE FILE

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👉 CESSNA PROGRESSIVE CARE

👉 CESSNA CUSTOMER CARE PROGRAM

👉 ALTERATIONS OR REPAIRS

👉 GROUND HANDLING TOWING

👉 PARKING

👉 TIE-DOWN

👉 JACKING

👉 LEVELING

👉 FLYABLE STORAGE

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